W DOC AIRBUS | AMM A320F

Special Detailed Inspection (HFEC) of Lateral Splicing, FR 11, LH/RH


TASK 53-11-00-220-807-A
Special Detailed Inspection (HFEC) of Lateral Splicing, FR 11, LH/RH


WARNING: BE CAREFUL WHEN YOU USE CONSUMABLE MATERIALS. OBEY THE MATERIAL MANUFACTURER'S INSTRUCTIONS AND YOUR LOCAL REGULATIONS.
ZONE: 211
ZONE: 212
1. Reason for the Job
Refer to the MPD TASK: 531127-01
SPECIAL DETAILED INSPECTION (HFEC) OF LATERAL SPLICING, FR 11, LH/RH
NOTE: The effectivity of this task is 'ALL'. To know if this task is applicable to your aircraft, refer to the MPD task applicability. The information on weight variant groups is given in the MPD and SRM introductions.
2. Job Set-up Information
 A. Consumable Materials
REFERENCE
DESIGNATION
(Material No.08BAA9)
Non Aqueous Cleaner-General - -
(Material No.14SBA1)
Textile-Lint free Cotton -
 B. Work Zones and Access Panels
ZONE/ACCESS
ZONE DESCRIPTION
211
COCKPIT
212
COCKPIT
 C. Referenced Information
REFERENCE
DESIGNATION
TASK 25-13-41-000-002-A
Removal of the Sidewall Panels
TASK 25-13-41-400-002-A
Installation of the Sidewall Panels
TASK 25-13-46-000-001-A
Removal of the Coat Stowage
TASK 25-13-46-400-001-A
Installation of the Coat Stowage
TASK 25-80-00-000-001-A
Removal of the Insulation Blankets
TASK 25-80-00-400-001-A
Installation of the Insulation Blankets
NTM 531127
SRM 511100
(for corrective action)
SRM 512200
(for corrective action)
3. Job Set-up
Subtask 53-11-00-010-113-A
A. Get Access
   (1) Remove the coat stowage, if installed. (Ref. AMM TASK 25-13-46-000-001).
   (2) Remove the necessary cockpit sidewall panels at FR 11 to get access to the inspection area (Ref. AMM TASK 25-13-41-000-002).
Subtask 53-11-00-020-074-A
B. Removal of the Components
   (1) Remove the necessary insulation blankets at FR 11 to get access to the inspection area (Ref. AMM TASK 25-80-00-000-001).
Subtask 53-11-00-110-132-A
C. Preparation of the Inspection Area
   (1) Make sure that the inspection area is sufficiently clean to do a satisfactory inspection of the area.
   (2) If not, clean the inspection area with Non Aqueous Cleaner-General - - (Material No.08BAA9) and a Textile-Lint free Cotton - (Material No.14SBA1) .
4. Procedure
Subtask 53-11-00-250-060-A
A. Inspection
   (1) Do a special detailed inspection of the structure of the splices at FR 11, on the left and right sides, for damage or discontinuities. Refer to Non-destructive Testing Manual ( NTM 531127).
   (2) Make a report of the damage after the NTM inspection:
     (a) Corrosion damage:
  • If you find corrosion, refer to the Structural Repair Manual ( SRM 512200) for the corrosion types, inspection, removal and subsequent corrosion protection.
     (b) Other damage (scratches, cracks, gouges, dents, creases):
  • If you find this type of damage, refer to the Structural Repair Manual ( SRM 511100) for damage types, classification and corrective action.
5. Close-up
Subtask 53-11-00-420-071-A
A. Installation of the Components
   (1) Install the insulation blankets at FR 11 (Ref. AMM TASK 25-80-00-400-001).
Subtask 53-11-00-410-113-A
B. Close Access
   (1) Install the cockpit sidewall panels at FR 11 (Ref. AMM TASK 25-13-41-400-002).
   (2) Install the coat stowage, if removed (Ref. AMM TASK 25-13-46-400-001).
   (3) Make sure that the work area is clean and clear of tools and other items.
[Rev.10 from 2021] 2026.04.02 06:28:45 UTC